CONTROLLER,ALTITUDE (P/N 2594775-200) - As Removed

The 2594775-200 is an altitude controller for aircraft autopilot and flight director systems. This avionics line-replaceable unit interfaces with the pitot-static system and AFCS to select, capture, and maintain target altitudes during flight. The controller processes altitude data and commands pitch control inputs to hold the preselected altitude automatically.

Installation requires verification against the aircraft illustrated parts catalog and compliance with avionics documentation and maintenance manual procedures. Commonly integrated into transport and business aircraft autopilot systems.

What is the CONTROLLER,ALTITUDE (P/N 2594775-200)?

The 2594775-200 is an altitude controller for aircraft autopilot and flight director systems. This avionics line-replaceable unit interfaces with the pitot-static system and AFCS to select, capture, and maintain target altitudes during flight.

Is the 2594775-200 compatible with my aircraft's avionics suite?

Avionics compatibility depends on your aircraft model and existing installation. The CONTROLLER,ALTITUDE is available in: As Removed. We recommend checking your aircraft's wiring diagrams and STC documentation, or contact our avionics team for compatibility assistance.

Does the 2594775-200 come with an 8130-3 airworthiness tag?

Availability of an FAA 8130-3 tag depends on the part condition. Overhauled and repaired units typically include 8130-3 documentation. As-removed units may include a removal tag with trace history. Contact us for specific documentation on the condition you need.

Do you offer bench testing for the 2594775-200?

We can arrange bench testing through our network of FAA-certified repair stations. Call (904) 998-9101 for testing availability and turnaround times, or submit an RFQ with your specific requirements.